• The Journal of Korean Institute of Communications and Information Sciences
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• v.37 no.7A
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• pp.503-511
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• 2012

In this paper, the performance analysis of telemetering method using delayed frame time diversity (DFTD) as the outer code and Reed-Solomon (RS) code as the inner code is described. DFTD is used to transmit a real-time frame together with a time-delayed frame which was saved in the memory during a defined period. The RS code as a kind of FEC (forward error correction) is serially concatenated with DFTD. This method was applied to the design of telemetry units that have been used for flight tests in a communication environment with deep fading. The data of the flight test for four cases with no applied code, with DFTD only, with the RS code only, and with both DFTD and the RS code are used to analyze the performance. The simulation for time-delay suggests the possibility that all frame errors can be removed. And the results of 12 flight tests show the performance superiority of this new method to compare with the RS code only.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.9
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• pp.760-770
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• 2012

In order to provide precision approach service based on GBAS, air navigation service providers should validate the GBAS system performance against international standard requirements and receive approval. The GBAS manufacturer should define integrity threat, analyze the integrity monitors and evaluate performance of the implemented monitors to verify integrity performance which is critical to the aircraft safety. This paper describes a statistical test result to evaluate performance of the code carrier divergence monitors implemented in KARI Integrity Monitor System software. The paper introduces analysis and test procedure which is developed for the performance evaluation and describes the analysis, the test scenario generation and the test results. The results show that the implemented monitors can detect the expected minimum detectable errors with satisfying the probability of missed detection requirements.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.05a
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• pp.133-136
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• 2003

우주발사체의 2단에 사용가능하며, 케로신과 액체산소를 추진제로 하는 10톤급 액체로켓엔진 (LRE)에 대해 노즐 설계 변수와 성능 특성과의 관계를 파악하고 노즐 성능의 개선을 위해 노즐 형상에 따른 성능 해석을 수행하였다. 본 연구에서 10톤급 LRE의 형상을 설계하였으며, 기존의 일차원 성능해석 방법과는 달리, 2차원 유동 해석 결과를 이용한 성능 해석을 수행하기 위해 노즐 성능해석용 코드를 개발하였으며, 액체 산소/메탄 엔진 (LNG 엔진)에 대한 지상 연소시험 결과와 비교, 검토하여 노즐 성능해석 코드를 검증하였다.

• 기계와재료
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• v.26 no.1
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• pp.50-62
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• 2014

원전발전소에 납품되는 원전용 안전밸브의 성능은 ASME나 KEPIC와 같은 기술기준코드에 따라 설정압력, 블로우다운(blowdown), 풀리프트(Full lift), 누설(leakage), 방출용량(discharge flow rate)등과 같은 특성인자로 평가된다. 그 중에서도 방출용량은 ASME SEC III NB 7000 코드에 따라 ASME 용량인증이 요구되지만, 아직 국내에는 국제적으로 공인되니 압력방출장치 용량시험기관이 부재하여 외화유출 및 국내 PRD 기술개발에 많은 어려움이 있어왔으며, 이에 따라 원전 PRD 인증기관 개발을 통하여 세계적인 인프라 구축의 필요성이 부각되고 있다. PRD 인증기관 구축은 국내 원전 핵심기자재의 고급기술 국산화에 이바지 할 수 있고, PRD 성능 및 용량시험지원을 통하여 국내 밸브기술 경쟁력 확보하는 데 기여할 것으로 기대된다.

• Journal of the Korea Institute of Information Security & Cryptology
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• v.28 no.3
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• pp.605-615
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• 2018

Due to the rapid growth of the Internet of Things market, the use of the C/C++ language, which is the most widely used language in embedded systems, is also increasing. To improve the quality of code in the C/C++ language and reduce development costs, it is better to use static analysis, a software verification technique that can be performed in the first half of the software development life cycle. Many programs use static analysis to verify software safety and many static analysis tools are being used and studied. In this paper, we use Clang static analysis tool to check security weakness detection performance of verified test code. In addition, we compared the static analysis results of the test codes applied with the source obfuscation techniques, layout obfuscation, data obfuscation, and control flow obfuscation techniques, and the static analysis results of the original test codes, Analyze the detection ability impact of the Clang static analysis tool.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2010.04a
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• pp.500-503
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• 2010

본 논문에서는 산업용 용접구조물의 피로성능 평가를 위한 시간 및 비용 절감형 전산피로시험법을 개발한다. 임의의 하중에 놓인 용접구조물의 성능저하 현상(균열발생 및 진전 등)을 손상역학에 기반하여 역학적으로 기술하고 자체개발한 유한요소해석코드에 탑재하여 이를 전산적으로 시뮬레이션한다. 정도 높은 용접구조물 전산피로시험법의 개발을 위해 용접잔류응력과 재료파라미터를 자체개발한 유한요소해석코드를 통해 구현한다. 개발된 전산피로시험법은 용접구조물의 피로시험 결과와 비교함으로서 제안 기법의 적합성 및 유용성을 검증한다.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.11a
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• pp.53-58
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• 1996

국내의 17$\times$17형 원전연료는 종전의 KOFA 연료로부터 Westinghouse(WH)사 Vantage-5H (V5H) 연료로 대체중에 있으며, 울진 1,2호기의 경우 8주기부터 V5H 연료를 장전한다. V5H 연료는 연료 상하부를 천연우라늄으로 구성함으로써 축방향 농축도가 균일하지 않으므로 기존 FRAMATOME사의 2차원 노심운전분석코드체계 (CEDRIC-CARIN-ESTHER)로는 정확한 노심 분석이 불가능하다. 따라서, 본 연구에서는 V5H 연료가 장전되는 울진 1,2호기에 대한 3차원 노심분석을 위하여 WH사의 INCORE-3D와 TOTE 코드를 PC-Version으로 개발하여 기존 코드체계를 대체하였다. 또한 WH형 원전과는 상이한 형식을 갖는 울진 1,2호기의 중성자속 측정 자료를 INCORE 코드에 적합한 형태로 변환하기 위한 C2I 코드를 개발하고 울진 1호기 6주기의 실제 중성자속 측정 자료를 이용하여 검증하였다. 이들 개발 코드들을 울진 원전에 설치하고, 1호기 8주기 출력상승중 노심출력분포 측정시험(75% 및 100% 출력시험)에 적용한 결과 기술지침서 상의 모든 제한사항이 만족되며 코드성능 또한 만족함을 확인하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.41-44
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• 2007

Ground test facility for the hypersonic propulsion system was designed, constructed and performance test was conducted. The design point was selected using quasi，1-Dimensional CFD analysis before the conceptual design for construction of hypersonic facility After that, specific designs for performance and components were completed using unit analysis CFD code and performance tests were conducted for the various operation conditions.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.4
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• pp.321-327
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• 2008

The shock tunnel as a hypersonic ground test facility was designed, constructed and its performance test was conducted to reproduce the high speed flow which the hypersonic propulsion system is encountered. The design points were understood and the conceptual design was completed using the quasi one dimensional operation analysis code. After that, the specific performance and compartment design were completed using CFD simulation as the part analysis. The facility was then constructed according to those design results and the performance test was conducted for various operation conditions. In this paper, we suggested the design method of hypersonic shock tunnel including the conceptual and performance design using theoretical analysis and the quasi 1D Multi-species computational fluid dynamics code.

• The Bulletin of The Korean Astronomical Society
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• v.17
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• pp.17.1-17.1
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• 1992